Compare rockets
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| Specification | Antares 110 Orbital Sciences Corporation × remove | Proton K/DM-2 Khrunichev State Research and Production Space Center × remove | Tsiklon-3 Yuzhnoye Design Bureau × remove |
|---|---|---|---|
| Flights | 2 | 110 | 122 |
| Success rate | 100% | 93.6% | 94.3% |
| Thrust | 3,265 kN | — | 2,713 kN |
| Height | 40.5 m | — | 39.27 m |
| Diameter | 3.9 m | — | 3 m |
| Launch mass | 276 t | — | 189 t |
| LEO capacity | 4,450 kg | — | 4,100 kg |
| GTO capacity | — | — | — |
| Launch cost | — | — | $15M |
| Reusable | No | No | No |
| Stages | 2 | — | 3 |